Fig. 19From: Adaptive wave-particle decomposition in UGKWP method for high-speed flow simulationsHypersonic flow at \({Ma} = 5\) and \({Kn} = 0.001\) around an Apollo reentry capsule. (a) Temperature and pressure distributions, and (b) local Knudsen Number \({Kn}_{Gll}\) distribution and Mach number along the streamlineBack to article page